Walter Regulus
From Wikipedia, the free encyclopedia
| Regulus | |
|---|---|
Walter Regulus II | |
| Type | Radial aero engine |
| National origin | Czechoslovakia |
| Manufacturer | Walter Aircraft Engines |
| First run | 1934 |
The Walter Regulus was a Czechoslovak five-cylinder, air-cooled radial engine for powering light aircraft that first ran in 1934. The engine produced 186 kW (250 hp).[1][2]
A preserved example of the Walter Regulus engine is on display at the following museum: